STMicroelectronics RHFAC14K1
- Part No.:
- RHFAC14K1
- Manufacturer:
- STMicroelectronics
- Category:
- Gates and Inverters
- Package:
- 14-CFlatPack
- Datasheet:
-
RHFAC14K1.pdf
- Description:
- RAD-HARD HEX SCHMITT INVERTER
- Quantity:
- Payment:

- Shipping:

Inventory:3,853
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Product details
Overview
RHFAC14K1 from STMicroelectronics is a radiation-hardened hex Schmitt-trigger inverter in the 54AC logic family, designed for aerospace and high-reliability systems requiring TID immunity up to 300 krad(Si), SEL immunity up to 110 MeV·cm²/mg, and operation from –55 °C to +125 °C. It supports CMOS-level input thresholds (2–6 V supply), delivers rail-to-rail output swing, and is housed in a QML-V qualified ceramic Flat-14 hermetic package.
For engineers reviewing the RHFAC14K1 datasheet, RHFAC14K1 pinout, RHFAC14K1 application, or RHFAC14K1 equivalent, this device is selected for critical timing conditioning, noise-immune signal inversion, and digital interface buffering in satellite command/data handling, radiation-tolerant FPGAs, and deep-space avionics where latch-up immunity and wide temperature stability are mandatory.
Technical Context
The RHFAC14K1 implements six independent Schmitt-trigger inverters with hysteresis (typically 0.8 V at VCC = 3 V), enabling robust noise rejection on slow or noisy input signals. Its input structure includes clamp diodes rated for ±20 mA, and outputs drive rail-to-rail with 3-state capability disabled (non-bus version).
It belongs to the AC-series subset optimized for low-power, high-speed CMOS operation across 2–6 V, distinct from the TTL-compatible ACT-series (4.5–5.5 V). Radiation hardening is achieved via process-level design (AMK6 diffusion line) and wafer-level qualification per MIL-STD-883 cond A.
Key Specifications
| Parameter | Value and Actual Design Meaning |
|---|---|
| VCC Range | 2 V to 6 V - Enables direct interfacing with mixed-voltage subsystems (e.g., 3.3 V FPGA I/O, 5 V legacy buses) |
| TID Hardness | 300 krad(Si) - Guaranteed functional operation after total ionizing dose exposure typical of LEO/GEO orbits |
| SEL Threshold | ≥110 MeV·cm²/mg - Immune to single-event latch-up under heavy-ion irradiation in space environments |
| Operating Temp | –55 °C to +125 °C - Validated performance across full military/aerospace thermal envelope without derating |
| Input Hysteresis | ≈0.8 V at VCC = 3 V - Provides ≥2× noise margin vs. standard CMOS inverters for reliable edge detection |
| Absolute Max VCC | 7 V - Allows safe transient overvoltage tolerance during power sequencing or ESD events |
Pinout & Package
Ceramic Flat-14 hermetic package (QML-V qualified), 14-terminal surface-mount outline with grounded metallic lid option. Dimensions: 9.27–9.73 mm × 6.19–6.50 mm × 2.31–2.72 mm (L × W × A), 1.27 mm pitch.
| Pin/Terminal | Circuit Role | Design Meaning |
|---|---|---|
| 1, 3, 5, 9, 11, 13 | Input (A1–A6) | CMOS-compatible Schmitt-trigger inputs; accept 0–VCC logic levels with hysteresis |
| 2, 4, 6, 10, 12, 14 | Output (Y1–Y6) | Full-rail CMOS outputs; drive loads up to ±20 mA with defined VOH/VOL across temperature |
| 7 | GND | Primary ground reference; electrically connected to lid in grounded-lid variants |
| 14 | VCC | Single positive supply; decoupling required within 10 mm for stable high-speed switching |
Key Features
| Feature | Design Value |
|---|---|
| Schmitt-trigger inputs | Enables clean signal regeneration from slow-rising or noisy waveforms (e.g., reset lines, sensor outputs) |
| 300 krad(Si) TID hardness | Eliminates need for periodic reconfiguration or redundancy in long-duration missions (e.g., planetary orbiters) |
| SEL immunity ≥110 MeV·cm²/mg | Prevents catastrophic latch-up failure during solar particle events without external current limiting |
| –55 °C to +125 °C operation | Supports unheated deployment in lunar night or uncooled electronics bays in launch vehicles |
| Hermetic ceramic packaging | Ensures zero moisture ingress and long-term reliability in vacuum or high-humidity terrestrial test environments |
Applications
| Spacecraft Telemetry Conditioning | Satellite Command Decoding |
|---|---|
|
Use Scenario: Converting analog-sourced telemetry signals (e.g., thermistor voltage ramps) into clean digital edges for ADC sampling and packetization. IC Role / Device Role / Timing Role: Signal conditioning front-end; provides hysteresis-based noise filtering and level translation between sensor domain and digital processing unit. Use Value: Eliminates false triggers caused by EMI in harnesses, ensuring accurate state reporting over multi-year missions without software debouncing overhead. |
Use Scenario: Validating received uplink commands prior to execution in fault-tolerant onboard computers. IC Role / Device Role / Timing Role: Input synchronizer and metastability filter; converts asynchronous command pulses into synchronized, glitch-free enable signals. Use Value: Prevents partial instruction execution during radiation-induced transients, maintaining command integrity without adding FPGA logic resources. |
| Rad-Hard FPGA Configuration Interface | Launch Vehicle Avionics Bus Isolation |
|
Use Scenario: Driving configuration clock and data lines to radiation-hardened FPGAs during power-on initialization. IC Role / Device Role / Timing Role: Clock buffer and data line inverter; ensures monotonic edge rates and impedance-matched drive into FPGA input capacitance. Use Value: Guarantees reliable bitstream loading under thermal cycling and ionizing radiation, avoiding configuration corruption or startup failures. |
Use Scenario: Isolating MIL-STD-1553 bus receivers from flight computer I/O pins in high-vibration launch phases. IC Role / Device Role / Timing Role: Level-shifting and noise-suppressing interface buffer; translates 1553 differential signals to single-ended CMOS logic. Use Value: Blocks ground-loop currents and RF coupling during ascent, preserving bus integrity without optocouplers or additional isolation ICs. |
Equivalent & Alternatives
The following parts are listed as comparable options for similar Schmitt-trigger inverter applications.
| Alternative Part | Technical Difference | Application Difference | Selection Advice |
|---|---|---|---|
| 54AC14 (non-K1 variant) | Same logic function and radiation specs, but not QML-V certified; lacks DLA SMD traceability and lot-level RHA documentation | Acceptable for ground-test or non-flight prototypes where formal qualification isn't mandated | Select only when formal space qualification (e.g., NASA Class B, ESA ECSS-Q-ST-60) is not required |
| RHFAC14A | Low-power variant (reduced ICC); identical radiation hardness and pinout, but higher propagation delay (typ. 9 ns vs. 7 ns at VCC = 3 V) | Better suited for battery-constrained subsystems where speed margin is relaxed (e.g., housekeeping monitors) | Choose when static power budget dominates over timing-critical paths |
Compared with RHFAC14K1, the 54AC14 offers cost savings without radiation certification, while RHFAC14A trades speed for lower quiescent current-making RHFAC14K1 optimal for flight-critical, speed-sensitive interfaces demanding full QML-V compliance.
Availability
RHFAC14K1 is available at Aetrix Electronics and suitable for spacecraft telemetry conditioning, satellite command decoding, rad-hard FPGA configuration, and launch vehicle avionics bus isolation requiring stable component supply under extended lead times and strict lot traceability.
Supply support for RHFAC14K1 includes scheduled delivery planning, volume procurement assistance, BOM continuity management, traceable sourcing, and lifecycle availability coordination for OEM customers, industrial embedded developers, connected-device designers, and electronics production programs.
Manufacturer
STMicroelectronics is a global semiconductor leader specializing in automotive, industrial, and aerospace-grade ICs, with decades of heritage in radiation-hardened technology and QML-V manufacturing.
RHFAC14K1 belongs to the 54ACxxxx rad-hard logic series, engineered specifically for mission-critical space electronics where immunity to total ionizing dose, single-event effects, and extreme thermal cycling is non-negotiable.
FAQ
Is RHFAC14K1 pin-compatible with commercial 74AC14 devices?
No. While logic function and pin numbering match, RHFAC14K1 uses a ceramic Flat-14 package with different mechanical dimensions, thermal characteristics, and hermetic sealing. Commercial 74AC14 parts use plastic DIP or SOIC packages and lack radiation hardening, making them unsuitable for space use even if footprint appears similar.
What is the maximum operating frequency of RHFAC14K1 at 3.3 V?
At VCC = 3.3 V and –55 °C to +125 °C, the typical propagation delay is 7 ns per inverter, supporting reliable operation up to ≈35 MHz for clean square-wave inputs. System-level frequency is limited by input transition time (dt/dv ≤ 8 ns/V) and load capacitance; derating is required above 25 MHz in high-radiation or high-temperature conditions.
Does RHFAC14K1 require external decoupling capacitors?
Yes. Each VCC pin must be decoupled with a minimum 100 nF X7R ceramic capacitor placed within 10 mm of the pin, plus a 1 µF bulk capacitor per package. This is mandatory to suppress switching noise and maintain stable operation under radiation-induced supply transients and thermal cycling.
Can the metallic lid be left floating, or must it be grounded?
The lid may be either floating or grounded per design requirements. In grounded-lid versions (e.g., RHFAC14K1-G), the lid connects internally to Pin 7 (GND); in floating-lid versions, no internal connection exists. Grounding improves EMI shielding and thermal conduction but requires mechanical grounding to PCB ground plane.
RHFAC14K1 Specifications
- Product attributes
- Attribute value
- Manufacturer:
- STMicroelectronics
- Series:
- 54AC
- Package/Case:
- 14-CFlatPack
- Packaging:
- Strip
- Product Status:
- Active
- Logic Type:
- Inverter
- Number of Circuits:
- 6
- Number of Inputs:
- 6
- Features:
- Schmitt Trigger
- Voltage - Supply:
- 2V ~ 6V
- Current - Quiescent (Max):
- -
- Current - Output High, Low:
- 50mA, 50mA
- Input Logic Level - Low:
- -
- Input Logic Level - High:
- -
- Max Propagation Delay @ V, Max CL:
- -
- Operating Temperature:
- -55°C ~ 125°C
- Grade:
- -
- Qualification:
- -
- Mounting Type:
- Surface Mount
- Supplier Device Package:
- 14-CFlatpack
RHFAC14K1 FAQ
1.How can I place an order for RHFAC14K1 through Aetrix?
Please submit a Request for Quotation (RFQ) for RHFAC14K1 on Aetrix. Our sales agent will provide a competitive quotation and guide you through the order confirmation once you accept the terms.
2.Are the price and stock information for RHFAC14K1 reliable?
The price and inventory of RHFAC14K1 are updated periodically and may fluctuate due to market conditions. Stock and pricing data are typically refreshed every 24 hours. Quotation validity for RHFAC14K1 is usually 5 days.
3.What payment methods are accepted for RHFAC14K1?
We accept Wire Transfer, PayPal, Credit Card, Western Union, MoneyGram, and Escrow for RHFAC14K1 transactions.
Note: Certain payment methods may incur a processing fee.
4.How is shipping managed for RHFAC14K1?
RHFAC14K1 orders can be shipped via leading logistics carriers, including DHL, UPS, FedEx, TNT, or Registered Mail.
Once your RHFAC14K1 order is processed, you will receive an email with the shipment details and tracking number.
Note: Tracking information may take up to 24 hours to appear. Express delivery typically takes 3–5 business days.
5.How can I obtain technical support or documentation for RHFAC14K1?
For technical support, including RHFAC14K1 datasheets, pinout diagrams, or application guidance, please contact our engineering support team. They can provide detailed documentation and assistance for your RHFAC14K1 requirements.
6.How does Aetrix verify that RHFAC14K1 is sourced from the original manufacturer or authorized distributors?
All RHFAC14K1 products on Aetrix are procured from qualified distributors and authorized channels. Our dedicated quality assurance team conducts strict verification, including traceability checks and, if necessary, third-party testing. This ensures that RHFAC14K1 meets industry standards.
7.What is the process for return or replacement of RHFAC14K1?
All RHFAC14K1 units undergo pre-shipment inspection (PSI). If there is an issue with RHFAC14K1, returns or replacements are accepted under the following conditions:
1.Quantity discrepancies, incorrect items, or visible external defects (such as breakage or corrosion), acknowledged by Aetrix.
2.The issue is reported within 90 days of delivery.
3.The RHFAC14K1 part is unused and in its original packaging.
Return procedure for RHFAC14K1:
1.Submit a request within 90 days.
2.Obtain a Return Material Authorization (RMA) from Aetrix.
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